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authorMarius Peter <blendoit@gmail.com>2019-06-29 15:23:02 -0700
committerMarius Peter <blendoit@gmail.com>2019-06-29 15:23:02 -0700
commit49dfbb065271bb3cc49daaac4ddf3b10c838a273 (patch)
tree6c4913f430a9bbdbc161b1dd012a3840ee30dfb1 /creator.py
parent2d792fd69a9d6306c78c346664761e22594e5a07 (diff)
doc
Diffstat (limited to 'creator.py')
-rw-r--r--creator.py6
1 files changed, 3 insertions, 3 deletions
diff --git a/creator.py b/creator.py
index d548c98..eaf4d68 100644
--- a/creator.py
+++ b/creator.py
@@ -15,10 +15,10 @@
"""
The creator.py module contains class definitions for coordinates
-and various components we add to an airfoil (spars, stringers, and ribs.)
+and various components we add to an airfoil (spars, stringers, and ribs).
Classes:
- Airfoil: instantiated with class method to provide coordinates to heirs
+ Airfoil: instantiated with class method to provide coordinates to heirs.
Spar: inherits from Airfoil.
Stringer: also inherits from Airfoil.
@@ -73,7 +73,7 @@ class Airfoil:
def add_naca(self, naca_num):
"""
- This function generates geometry for our chosen NACA airfoil shape.
+ This function generates geometry for a NACA number passed as argument.
The nested functions perform the required steps to generate geometry,
and can be called to solve the geometry y-coordinate for any 'x' input.
Equation coefficients were retrieved from Wikipedia.org.
Copyright 2019--2024 Marius PETER